# Service difficulty reports: N754SW, cancelled Oct 4, 2024

A list on [N754SW, cancelled Oct 4, 2024](https://openairdocs.org/deregistered/N754SW-2024-10-04.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 6 · 298 reports

- [SDR SWAA2023071176799](https://openairdocs.org/sdr/SWAA2023071176799.md): Battery Pack · inoperative · Jul 10, 2023 · N754SW · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS AT ROWS 9ABC; 12ABC; AND 14ABC INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT POSITION M1670 PER AMM 33-51-06
- [SDR SWAA2023070674450](https://openairdocs.org/sdr/SWAA2023070674450.md): Pressure System · faulted · Jul 2, 2023 · N754SW · Boeing 7377H4 · Cabin Pressure Control System
  > LOSS OF CABIN PRESSURE AT 36K FEET EMERGENCY DESCENT PERFORMED CABIN ALT WARNING HORN SOUNDED PAX OXY MASKS DEPLOYED. EMERGENCY DECLARED LANDING UNEVENTFUL. ACCOMPLISHED CABIN DEPRESSURIZATION CONDITIONAL INSP IAW AMM 05-51-81 WITH NO DEFECTS NOTED. ACCOMPLI
- [SDR SWAA2023062370585](https://openairdocs.org/sdr/SWAA2023062370585.md): Cover · out of adjust · Jun 22, 2023 · N754SW · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY DOOR EXIT LIGHT COVER CAME OFF<[01] INSTALLED COVER AS PER SIP.
- [SDR SWAA2023061959880](https://openairdocs.org/sdr/SWAA2023061959880.md): Flap · delaminated · Jun 16, 2023 · N754SW · Boeing 7377H4 · Trailing Edge Flap Control System
  > LH OUTBOARD AFT FLAP IS DELAMINATED ON INBOARD AFT CORNER DELAMINATION MEASURES APRROX 1.25IN BY 4.5IN ON LOWER SKIN<[01] VERIFIED THE DAMAGE RECORD ENTERED; AND CORRECT SRM REFERENCE WAS SELECTED WITH CORRECT FOLLOW-ON PARAMETERS.;[02] DAMAGE ALLOWABLE REF SR
- [SDR SWAA2023061959881](https://openairdocs.org/sdr/SWAA2023061959881.md): Flap · delaminated · Jun 16, 2023 · N754SW · Boeing 7377H4 · Trailing Edge Flap Control System
  > RH OUTBOARD AFT FLAP IS DELAMINATED ON INBOARD AFT CORNER DELAMINATION MEASURES APRROX 2IN BY 3.5IN ON UPPER SKIN<[01] VERIFIED THE DAMAGE RECORD ENTERED; AND CORRECT SRM REFERENCE WAS SELECTED WITH CORRECT FOLLOW-ON PARAMETERS.;[02] DAMAGE ALLOWABLE REF SRM 5
- [SDR SWAA2023013196494](https://openairdocs.org/sdr/SWAA2023013196494.md): Girt Bar · damaged · Jan 28, 2023 · N754SW · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE GIRT BAR MISSING STOP RING<[01] INSTALLED MISSING FWD ENTRY DOOR SLIDE GIRT BAR STOP RING IAW AMM 25-66-01.
- [SDR SWAA2023013196493](https://openairdocs.org/sdr/SWAA2023013196493.md): Sign · damaged · Jan 28, 2023 · N754SW · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN FELL OFF AT L1 DOOR<[01] RE-INSTALLED EXIT SIGN PER SIP
- [SDR SWAA2022120176659](https://openairdocs.org/sdr/SWAA2022120176659.md): Fairing · damaged · Nov 30, 2022 · N754SW · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > FOUND 2 LOCK FASTENER HOLES ON THE LT STRUT FAIRING ELONGATED ON THE LT SIDE. REPAIRED THE DAMAGEIAW EA 22-154-03528.
- [SDR SWAA2022092830341](https://openairdocs.org/sdr/SWAA2022092830341.md): Panel · damaged · Sep 26, 2022 · N754SW · Boeing 7377H4 · Fuselage Main, Structure
  > 193B FASTENER HOLES AT POSITIONS 7; 8; 18; 20; 25; 26 AND 33 HAVE BEEN ELONGATED. 193B FASTENER HOLES AT POSITIONS 7 8 18 20 25 26 AND 33 HAVE BEEN ELONGATED. / [01] PANEL REPLACED ON N/R TTG8Q00F0UYM;[02] C/W
- [SDR SWAA2022092283045](https://openairdocs.org/sdr/SWAA2022092283045.md): Slide · out of position · Sep 18, 2022 · N754SW · Boeing 7377H4 · Escape Slide
  > L1 DOOR SLIDE NEEDS REPOSITIONED / [01] REPOSITIONED L1 DOOR SLIDE PER S.I.P.
- [SDR SWAA2022081240386](https://openairdocs.org/sdr/SWAA2022081240386.md): Cover · loose · Aug 10, 2022 · N754SW · Boeing 7377H4 · Escape Slide
  > RIGHT AFT ESCAPE SLIDE PULL STRAP IS NOT SECURED. / [01] RESECURED AFT RH ESCAPE SLIDE PULL STRAP COVER AS REQUIRED PER SIP.
- [SDR SWAA2022052309686](https://openairdocs.org/sdr/SWAA2022052309686.md): Megaphone · failed · May 19, 2022 · N754SW · Boeing 7377H4 · Emergency Equipment
  > FWD GALLEY MEGAPHONE BATTERY IS DEPLETED / [01] R&R FWD MEGAPHONE AS NEEDED AMM 25-64-00. OPS CHK GOOD.
- [SDR SWAA2022052310324](https://openairdocs.org/sdr/SWAA2022052310324.md): Megaphone · failed · May 19, 2022 · N754SW · Boeing 7377H4 · Emergency Equipment
  > FWD GALLEY MEGAPHONE BATTERY IS DEPLETED / [01] R&R FWD MEGAPHONE AS NEEDED AMM 25-64-00. OPS CHK GOOD.
- [SDR SWAA2021091010655](https://openairdocs.org/sdr/SWAA2021091010655.md): Rib · cracked · Aug 24, 2021 · N754SW · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK LEADING EDGE SKIN ACCESS PANEL 341B AT STA 95.96 AT RT HORIZONTAL STABILIZER (1 EA); 2021-368797 / [01] TOOK MEASURES OF CRACK RIB LEADING EDGE SKIN ACCESS PANEL 241B AT STA 95.96 RT HORIZONTAL STABILIZER MEASURES ARE: L:0.245 TOOL USED IS CALIPER P/N:
- [SDR SWAA2021091010656](https://openairdocs.org/sdr/SWAA2021091010656.md): Rib · cracked · Aug 24, 2021 · N754SW · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK LEADING EDGE SKIN ACCESS PANEL 341B AT STA 105.26 AT RT HORIZONTAL STABILIZER (1 EA); 2021-368798 / [01] TOOK MEASURES OF CRACK RIB LEADING EDGE SKIN ACCESS PANEL 241B AT STA 105.26 AT RT HORIZONTAL STABILIZER MEASURES ARE: L:0.235 TOOL USED IS CALIPER
- [SDR SWAA2021091007193](https://openairdocs.org/sdr/SWAA2021091007193.md): Rib · cracked · Aug 13, 2021 · N754SW · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER; 2021-368760 / [01] TOOK MEASURE OF CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IS L: 0.452 AND NO FOUND ALLOWA
- [SDR SWAA2021091007194](https://openairdocs.org/sdr/SWAA2021091007194.md): Angle · cracked · Aug 13, 2021 · N754SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE AT PLENUM RT APU AIR INLET; 2021-368759 / [01] REMOVED ANGLE AND FASTENERS AT PLENUM RT APU AIR INLET IAW B737-700 SRM 51-40-02 AND PERFORMED VISUEL INSPECTION AND NOT FOUND MORE DAMAGE ON ADJACENT AREA AND DUE TO NOT FOUN ALLOWABLE DAMAGE ANGL
- [SDR SWAA2021091005853](https://openairdocs.org/sdr/SWAA2021091005853.md): Support Angle · cracked · Aug 11, 2021 · N754SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK FRONT SPAR SUPPORT ANGLE LOCATED AT IFSS 120 AT LT WING; 2021-368744 / [01] REMOVED SUPPORT ANGLE LOCATED FRONT SPAR WEB AT IFSS 120 AT LT WING IAW B737-700 SRM 51-40-02 DUE TO NOT FOUND ALLOWBLE DAMAGE IN SRM SUPPORT ANGLE MUST BE REPLACED; CRACK LENG
- [SDR SWAA2021091005852](https://openairdocs.org/sdr/SWAA2021091005852.md): Spar · corroded · Aug 11, 2021 · N754SW · Boeing 7377H4 · Wing Spar
  > CORROSION FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APPROX; LOWER AREA AT LT WING; 2021-368745 / [01] TOOL USED/ EDDY CURRENT PN/ NORTEC 600D; SN/ 2000053402; DUE DATE/ 23APR22.; [02] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN/ 25DL PLUS;SN/ 071504410;
- [SDR SWAA2021091005851](https://openairdocs.org/sdr/SWAA2021091005851.md): Scuff Plate · cracked · Aug 10, 2021 · N754SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARMENT; 2021-368743 / [01] WELDED CRACKS LOCATED AT FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I.A.W BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B. STEP (4) AND BAC 5975 WELD ROD USED: AMS 4190K P.O
- [SDR SWAA2021091005435](https://openairdocs.org/sdr/SWAA2021091005435.md): Support Angle · cracked · Aug 9, 2021 · N754SW · Boeing 7377H4 · Galley Doors
  > CRACK ANGLE - SUPPORT ON ACCESS PANEL 834DZ AFT ENTRY DOOR AT AFT GALLEY AREA; 2021-368699 / [01] REMOVED ANGLE LOC. ON ACCESS PANEL 834DZ AFT ENTRY DOOR AT AFT GALLEY AREA IAW 737-700 SRM 51-40-02 ANGLE MUST BE REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE LIMI
- [SDR SWAA2021091005436](https://openairdocs.org/sdr/SWAA2021091005436.md): Support Angle · cracked · Aug 9, 2021 · N754SW · Boeing 7377H4 · Service Doors
  > CRACK ANGLE - SUPPORT ON ACCESS PANEL 844DZ AFT SERVICE DOOR AT AFT GALLEY AREA; 2021-368698 / [01] REMOVED ANGLE LOC. ON ACCESS PANEL 844DZ AFT SERVICE DOOR AT AFT GALLEY AREA IAW 737-700 SRM 51-40-02 ANGLE MUST BE REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE
- [SDR SWAA2021091004683](https://openairdocs.org/sdr/SWAA2021091004683.md): Stub Frame · cracked · Aug 8, 2021 · N754SW · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON STUB FRAME LOCATED AT BS 294.5 AT LEVEL STR 9R FWD GALLEY DOOR AREA; 2021-368691 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 21-JAN-22; [02] REPLACED STUB FRAME LOC. BS 294.5 AT LEVEL STR 9R FWD GALLEY DOOR IAW
- [SDR SWAA2021091004682](https://openairdocs.org/sdr/SWAA2021091004682.md): Angle · cracked · Aug 7, 2021 · N754SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS 827 STR 25R AT AFT CARGO COMPARTMENT; 2021-368685 / [01] REMOVED ANGLE - SUPPORT LOCATED BS 827 STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0; ANGLE SUPPORT MUST BE REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE
- [SDR SWAA2021091004676](https://openairdocs.org/sdr/SWAA2021091004676.md): Scuff Plate · cracked · Aug 7, 2021 · N754SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CUSTOMER REQUEST CRACK SCUFF PLATE FWD CORNER FWD ENTRY DOOR AT FWD GALLEY AREA; 2021-368687 / [01] EVALUATED SCUFF PLATE FWD CORNER FWD ENTRY DOOR AT FWD GALLEY AREA FOUND CRACK (1EA) MEASURE IS:L=0.4300 INCH.THE CRACK MUST BE REPAIR IAW BOEING 737-700 SRM 5
- [SDR SWAA2021091004679](https://openairdocs.org/sdr/SWAA2021091004679.md): Scuff Plate · cracked · Aug 7, 2021 · N754SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CUSTOMER REQUEST CRACK SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA; 2021-368684 / [01] EVALUATED SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA FOUND CRACKS (4EA) MEASURES ARE #1=1.4390 INCH;#2=2.2750 INCH;#3=2.5025 INCH;#4=1.8400 INCH;THESES CRACKS MUST
- [SDR SWAA2021091004678](https://openairdocs.org/sdr/SWAA2021091004678.md): Angle · cracked · Aug 7, 2021 · N754SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BETWEEN BS 907 TO BS 927 AND STR 27R TO STR 25R FWD POSITION AFT CARGO COMPARTMENT; 2021-368686 / [01] TOOK MEASURE OF CRACK ON SUPPORT ANGLE: L=5.854 TOOL USED: CAPLIPER P/N: DIGITAL 150; S/N: AE-412597; DUE DATE: 25-MAY-22 NOT
- [SDR SWAA2021091004681](https://openairdocs.org/sdr/SWAA2021091004681.md): Support Angle · cracked · Aug 7, 2021 · N754SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BETWEEN BS 907 TO BS 927 AND STR 25R TO STR 27R AFT POSITION AFT CARGO COMPARTMENT; 2021-368689 / [01] TOOK MEASURE OF CRACK ON SUPPORT ANGLE: L=3.465 TOOL USED: CAPLIPER P/N: DIGITAL 150; S/N: AE-412597; DUE DATE: 25-MAY-22 NOT
- [SDR SWAA2021091004680](https://openairdocs.org/sdr/SWAA2021091004680.md): Scuff Plate · cracked · Aug 7, 2021 · N754SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CUSTOMER REQUEST CRACK SCUFF PLATE AFT CORNER FWD ENTRY DOOR AT FWD GALLEY AREA; 2021-368688 / [01] EVALUATED AFT CORNER SCUFF PLATE AT FWD ENTRY DOOR GALLEY AREA FOUND CRACK (1EA) MEASURE IS:L=01450 INCH;THE CRACK IS WITHIN LIMIT OF REPAIR IAW BOEING 737-700
- [SDR SWAA2021091003820](https://openairdocs.org/sdr/SWAA2021091003820.md): Pressure Deck · cracked · Aug 5, 2021 · N754SW · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK WEB PRESSURE DECK HORIZONTAL AT MAIN WHEEL WELL COMPARTME (2 EA) (CRACK 1 LOC. AT RBL 41 AND BS 663; L= 1.125 INCH APPROX; AND CRACK 2 LOC. AT RBL 42 AND BS 675; L= 1 INCH APPROX); 2021-368568 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC500D; S
- [SDR SWAA2021091003792](https://openairdocs.org/sdr/SWAA2021091003792.md): Support Angle · cracked · Aug 5, 2021 · N754SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS 695 AND BL0 LH SIDE AT PASSENGER CABIN; 2021-368563 / [01] REMOVED SUPPORT ANGLE LOC. BS 695 AND BL0 LH SIDE AT PASSENGER CABIN IAW SRM B737-700 SRM-51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700; ANGLE MUST BE REPLA
- [SDR SWAA2021091004665](https://openairdocs.org/sdr/SWAA2021091004665.md): Support Angle · cracked · Aug 5, 2021 · N754SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED ON BS540 AND BL0 TO LBL24.5 AT PASSENGER CABIN; 2021-368610 / [01] REPLACED SUPPORT ANGLE LOCATED ON BS540 AND BL0 TO LBL24.5 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 STEP 9; SRM 51-40-02 AND DWG 143A5240 SHEET 1 REV -; [02] R
- [SDR SWAA2021091003819](https://openairdocs.org/sdr/SWAA2021091003819.md): Rib · cracked · Aug 5, 2021 · N754SW · Boeing 7377H4 · Vertical Stabilizer, Spar/Rib
  > CRACK DORSAL FIN RIB FWD POSITION AT VERTICAL STABILIZER; 2021-368570 / [01] REMOVED RIB LOC. DORSAL FIN FWD POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 DUE TO NOT FOUND ALLOWED DAMAGE ON SRM; RIB MUST BE REPLACED CRACK LENGTH IS: 0.625 TOOL U
- [SDR SWAA2021091011165](https://openairdocs.org/sdr/SWAA2021091011165.md): Bracket · cracked · Aug 5, 2021 · N754SW · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > CRACK OUTBOARD FAN COWL SUPPORT BRACKET LOC. INTERNAL AREA ACCESS DOOR 424AR ON ENGINE 2; 2021-368631 / [01] MEASURED OF CRACK OUTBOARD FAN COWL SUPPORT BRACKET LOC. INTERNAL AREA ACCESS DOOR 424AR ON ENGINE 2. L: 0.625 INCH TOOL USED P/N: 500-172-30; S/N: 15
- [SDR SWAA2021091003811](https://openairdocs.org/sdr/SWAA2021091003811.md): Bear Strap · cracked · Aug 5, 2021 · N754SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK INDICATION FOUND AROUND FASTENERS ON BEAR STRAP (2EA) LOCATED BETWEEN BS 293 TO BS 293.5 AND BETWEEN STR 8 AND STR 9 RH SIDE IN FWD GALLEY AREA LENGTH (1) CRACK 0.260 INCH; LENGTH (2) CRACK IS 0; 2021-368567 / [01] TOOL USED P/N: NORTEC 500D; S/N: N500X
- [SDR SWAA2021091003789](https://openairdocs.org/sdr/SWAA2021091003789.md): Support Bracket · cracked · Aug 4, 2021 · N754SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK SUPPORT BRACKET TRAILING EDGE DEFLECTION CONTROL RIB ORSS 271 AT LT WING; 2021-368553 / [01] REMOVED SUPPORT BRACKET TRAILING EDGE DEFLECTION CONTROL RIB ORSS 271 AT LT WING IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON AREA NOT FOUND MOR
- [SDR SWAA2021091003784](https://openairdocs.org/sdr/SWAA2021091003784.md): Angle · cracked · Aug 4, 2021 · N754SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 RT WING; 2021-368530 / [01] REMOVED ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 RT WING IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON AREA NOT FOUND MORE DAMAGE DUE TO NOT
- [SDR SWAA2021091003801](https://openairdocs.org/sdr/SWAA2021091003801.md): Support Angle · cracked · Aug 4, 2021 · N754SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS 695 AND BL0 RH SIDE AT PASSENGER CABIN; 2021-368562 / [01] REMOVED SUPPORT ANGLE LOC. BS 695 AND BL0 RH SIDE AT PASSENGER CABIN IAW SRM B737-700 SRM-51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700; ANGLE MUST BE REPLA
- [SDR SWAA2021091003382](https://openairdocs.org/sdr/SWAA2021091003382.md): Light · broken · Aug 3, 2021 · N754SW · Boeing 7377H4 · Emergency Lighting
  > BROKEN GALLEY 1 EMERGENCY LIGHT ASSY AND LENS AT FWD GALLEY AREA; 2021-368307 / [01] REPLACED GALLEY 1 EMERGENCY LIGHT ASSY AND LENS AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802.; [02] TASK CARD COMPLETED
- [SDR SWAA2021091003380](https://openairdocs.org/sdr/SWAA2021091003380.md): Scuff Plate · cracked · Aug 3, 2021 · N754SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT; 2021-368319 / [01] TOOL USED; DIGITAL CALIPER P/N:500-197-30 S/N: B20189526 DUE DATE 22-NOV-21; [02] REPAIRED BY WELD FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-30-15-2R-
- [SDR SWAA2021091003393](https://openairdocs.org/sdr/SWAA2021091003393.md): Rib · cracked · Aug 3, 2021 · N754SW · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER; 2021-368396 / [01] TOOK MEASURE OF CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IS L: 0.435. AND NO FOUND ALLOW
- [SDR SWAA2021091003381](https://openairdocs.org/sdr/SWAA2021091003381.md): Spar · corroded · Aug 3, 2021 · N754SW · Boeing 7377H4 · Wing Spar
  > CORROSION FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APPROX AT LT WING; 2021-368354 / [01] TOOL USED/ EDDY CURRENT PN/ NORTEC 600D; SN/ 2000053402; DUE DATE/ 23APR22.; [02] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN/ 25DL PLUS;SN/ 071504410; DUE DATE/ 20
- [SDR SWAA2021091003396](https://openairdocs.org/sdr/SWAA2021091003396.md): Bulkhead Web · cracked · Aug 3, 2021 · N754SW · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CUSTOMER REQUEST CRACK BODY STATION 663.75 VAPOR BARRIER APPROX LBL 14 AT MAIN WHEEL WELL COMPARTMENT; 2021-368398 / [01] TOOL USED CALIPER: P/N:500-197-20 S/N:13083235 DUE DATE:18-AUG-21.; [02] HOT BONDER P/N HCS9200B-AV S/N 18196127 DUE DATE 11-DEC-21; [03]
- [SDR SWAA2021091003394](https://openairdocs.org/sdr/SWAA2021091003394.md): Rib · cracked · Aug 3, 2021 · N754SW · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER; 2021-368397 / [01] TOOK MEASURE OF CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IS L: 0.435 NO FOUND ALLOWABLE
- [SDR SWAA2021091002930](https://openairdocs.org/sdr/SWAA2021091002930.md): Access Panel · cracked · Aug 2, 2021 · N754SW · Boeing 7377H4 · Aerodynamic Fairings
  > CRACK ACCESS PANEL 194E BODY FAIRING FASTENER HOLES AT LOWER FUSELAGE; 2021-368288 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: B17030925; DUE DATE: 06-AUG-21.; [02] TOOL USE SCALE: P/N: SCA-301; S/N:AE-412130; DUE DATE: 24-FEB-22.; [03] TOOL USED: HOT BONDER
- [SDR SWAA2021091002931](https://openairdocs.org/sdr/SWAA2021091002931.md): Access Panel · cracked · Aug 2, 2021 · N754SW · Boeing 7377H4 · Aerodynamic Fairings
  > CRACK ACCESS PANEL 193D BODY FAIRING HOLES AT LOWER FUSELAGE; 2021-368286 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: B17030925; DUE DATE: 06-AUG-21.; [02] TOOL USE SCALE: P/N: SCA-301; S/N:AE-412130; DUE DATE: 24-FEB-22.; [03] TOOL USED P/N: FLUKE87-5. S/N:
- [SDR SWAA2021091000852](https://openairdocs.org/sdr/SWAA2021091000852.md): Access Panel · broken · Aug 2, 2021 · N754SW · Boeing 7377H4 · Aerodynamic Fairings
  > BROKEN ACCESS PANEL 192BR WING TO BODY FAIRING STUDS AT LOWER FUSELAGE (8 EA); 2021-368265 / [01] REPLACED STUDS ACCESS PANEL 192BR WING TO BODY FAIRING AT LOWER FUSELAGE (8 EA) IAW B737-700 SRM 51-40-02-0G; [02] REPLACED STUDS ACCESS PANEL 192BR WING TO BODY
- [SDR SWAA2021091000853](https://openairdocs.org/sdr/SWAA2021091000853.md): Floor Panel · broken · Aug 2, 2021 · N754SW · Boeing 7377H4 · Fuselage Floor Panel
  > BROKEN FLOOR PANEL 140CF SPLICE PLATE FWD CUT OUT OF DOOR AT AFT CARGO COMPARTMENT; 2021-368266 / [01] REPLACED PANEL 140CF SPLICE PLATE FWD CUT OUT OF DOOR AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 PART NUMBER USED 453A2611-1 PO 2020 181966;
- [SDR SWAA2021071994278](https://openairdocs.org/sdr/SWAA2021071994278.md): Stiffener · cracked · Jul 13, 2021 · N754SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > STIFFENER CRACKED; DIAGONAL STIFFENER CRACKED IN LH AC BAY LOCATED ON WING CENTER SECTION REAR SPAR FIBERGLASS VAPOR BARRIER BETWEEN LBL 6.15 AND LBL 31.83. / [01] REMOVED CRACKED STIFFENER. LOCATED; DRILLED AND INSTALLED NEW STIFFENER PER SRM 51-40-02.; [02]
- [SDR SWAA2021071994280](https://openairdocs.org/sdr/SWAA2021071994280.md): Pressure Deck · cracked · Jul 13, 2021 · N754SW · Boeing 7377H4 · Fuselage Main, Structure
  > VAPOR BARRIER INTERIM REPAIR APPLIED PER SRM 51-10-10-1A-2; APPLIED INTERIM SEAL OVER THE CRACK AT LBL 11.9; 45 FROM PRESSURE DECK THA IN PER SRM 57 -10-10 PARAGRAPH 2.C.(4)/ALLOWABLE DAMAGE 2. VISUAL INSPECTION REQUIRED OF THE REPAIR AREA AT 1200 FLIGHT CYCK

Next page: https://openairdocs.org/deregistered/N754SW-2024-10-04/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N754SW' AND deregistration_id = 'N754SW-2024-10-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N754SW-2024-10-04/reports

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